FIELD: aircraft engineering.
SUBSTANCE: rotor is spinned at minimum common pitch to preset rpm at starting. Then, craft vertical lift is performed till undercarriages wheels rotation by increase of common pitch and rotor thrust. Thereafter, it is accelerated by changing the engine control levers into takeoff position till preset takeoff speed and altitude.
EFFECT: takeoff without jump.
Title | Year | Author | Number |
---|---|---|---|
HIGH-SPEED ROTORCRAFT | 2014 |
|
RU2573698C2 |
METHOD OF LANDING ROTORCRAFT WITHOUT ALIGHTING RUN WITH AUTOROTATING ROTOR AND WING | 2013 |
|
RU2506203C1 |
ROTOR-CRAFT | 2016 |
|
RU2662339C2 |
ROTOR "AIR WHEEL", GYROSTABILISED AIRCRAFT AND WIND-DRIVEN ELECTRIC PLANT USING ROTOR "AIR WHEEL", SURFACE/DECK DEVICES FOR THEIR START-UP | 2013 |
|
RU2538737C9 |
AUTOGYRO WITH POSSIBILITY OF VERTICAL TAKE-OFF | 2017 |
|
RU2674743C1 |
AIRCRAFT | 2022 |
|
RU2797468C1 |
MULTI-SCREW UNMANNED ROTORCRAFT | 2016 |
|
RU2611480C1 |
HEAVY-DUTY MULTIROTOR CONVERTIBLE ROTORCRAFT | 2013 |
|
RU2521121C1 |
GYROPLANE | 2018 |
|
RU2673933C1 |
HIGH-SPEED TURBOFAN COMBINED HELICOPTER | 2016 |
|
RU2629475C1 |
Authors
Dates
2014-04-27—Published
2013-01-23—Filed